The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 04, 2018

Filed:

Oct. 11, 2013
Applicant:

Techspace Aero S.a., Herstal, BE;

Inventor:

Christophe Remy, Fexhe-le-Haut-Clocher, BE;

Assignee:

SAFRAN AERO BOOSTERS SA, Herstal (Milmort), BE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/30 (2006.01); F01D 5/32 (2006.01);
U.S. Cl.
CPC ...
F01D 5/14 (2013.01); F01D 5/3038 (2013.01); F01D 5/32 (2013.01); Y02T 50/671 (2013.01);
Abstract

The subject application relates to blade root wedging lock in a circumferential groove in a rotor such as the drum of an axial turbomachine compressor. The body () of the lock includes a solid portion () designed to be housed in the groove and having two opposite bearing surfaces () and at least one circumferential wedging surface (). The body () further includes an upper portion () in the shape of an elongated generally vertical chamber designed to be flush with the upper surfaces of the platforms of adjacent blades when the lock is correctly positioned. This chamber () is truncated () so as to reduce its length in a direction perpendicular to the circumference, corresponding to the axis of rotation of the rotor. The lock can thus be accommodated in a narrow groove without decreasing the diameter of the clamping screw passing through the hole (). The subject application also relates to a rotor and a turbomachine equipped with the lock.


Find Patent Forward Citations

Loading…